Encyclopedia Astronautica
HYSR-1


Lox/Solid propellant rocket stage. Thrust 270.00 kN.

Status: Retired 2002.
Height: 15.00 m (49.00 ft).
Diameter: 0.61 m (2.00 ft).
Thrust: 270.00 kN (60,690 lbf).

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Associated Countries
Associated Engines
  • HYSR LMSS Lox/Solid hybrid rocket engine. 270 kN. More...

Associated Launch Vehicles
  • HYSR American sounding rocket. Hybrid single stage rocket intended to replace multiple-stage sounding rockets. More...

Associated Manufacturers and Agencies
  • Lockheed American manufacturer of rockets, spacecraft, and rocket engines. Lockheed Martin, Sunnyvale, CA, USA. More...

Associated Propellants
  • Lox/Solid Liquid oxygen was the earliest, cheapest, safest, and eventually the preferred oxidiser for large space launchers. Its main drawback is that it is moderately cryogenic, and therefore not suitable for military uses where storage of the fuelled missile and quick launch are required. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

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